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Document Outline

• Front Matter
• Preface
• Table of Contents
• 1. Classification
  • 1.1. Duct Jet Propulsion
  • 1.2. Rocket Propulsion
  • 1.3. Applications of Rocket Propulsion
  • References
• 2. Definitions and Fundamentals
  • 2.1. Definitions
  • 2.2. Thrust
  • 2.3. Exhaust Velocity
  • 2.4. Energy and Efficiencies
  • 2.5. Typical Performance Values
  • Problems
  • Symbols
  • References
• 3. Nozzle Theory and Thermodynamic Relations
  • 3.1. Ideal Rocket
  • 3.2. Summary of Thermodynamic Relations
  • 3.3. Isentropic Flow through Nozzles
  • 3.4. Nozzle Configurations
  • 3.5. Real Nozzles
  • 3.6. Four Performance Parameters
  • 3.7. Nozzle Alignment
  • 3.8. Variable Thrust
  • Problems
  • Symbols
  • References
• 4. Flight Performance
  • 4.1. Gravity-Free Drag-Free Space Flight
  • 4.2. Forces Acting on a Vehicle in the Atmosphere
  • 4.3. Basic Relations of Motion
  • 4.4. Effect of Propulsion System on Vehicle Performance
  • 4.5. Space Flight
  • 4.6. Flight Maneuvers
  • 4.7. Flight Vehicles
  • 4.8. Military Missiles
  • 4.9. Aerodynamic Effect of Exhaust Plumes
  • 4.10. Flight Stability
  • Problems
  • Symbols
  • References
• 5. Chemical Rocket Propellant Performance Analysis
  • 5.1. Background and Fundamentals
  • 5.2. Analysis of Chamber or Motor Case Conditions
  • 5.3. Analysis of Nozzle Expansion Processes
  • 5.4. Computer Analysis
  • 5.5. Results of Thermochemical Calculations
  • Problems
  • Symbols
  • References
• 6. Liquid Propellant Rocket Engine Fundamentals
  • 6.1. Propellants
  • 6.2. Propellant Feed Systems
  • 6.3. Gas Pressure Feed Systems
  • 6.4. Propellant Tanks
  • 6.5. Tank Pressurization
  • 6.6. Turbopump Feed Systems and Engine Cycles
  • 6.7. Flow and Pressure Balance
  • 6.8. Rocket Engines for Maneuvering, Orbit Adjustments, or Attitude Control
  • 6.9. Valves and Pipe Lines
  • 6.10. Engine Support Structure
  • Problems
  • Symbols
  • References
• 7. Liquid Propellants
  • 7.1. Propellant Properties
  • 7.2. Liquid Oxidizers
  • 7.3. Liquid Fuels
  • 7.4. Liquid Monopropellants
  • 7.5. Gelled Propellants
  • 7.6. Gaseous Propellants
  • 7.7. Safety and Environmental Concerns
  • Problems
  • Symbols
  • References
• 8. Thrust Chambers
  • 8.1. Injectors
  • 8.2. Combustion Chamber and Nozzle
  • 8.3. Heat Transfer Analysis
  • 8.4. Starting and Ignition
  • 8.5. Variable Thrust
  • 8.6. Sample Thrust Chamber Design Analysis
  • Problems
  • Symbols
  • References
• 9. Combustion of Liquid Propellants
  • 9.1. Combustion Process
  • 9.2. Analysis and Simulation
  • 9.3. Combustion Instability
  • Problems
  • References
• 10. Turbopumps, Engine Design, Engine Controls, Calibration, Integration, and Optimization
  • 10.1. Turbopumps
  • 10.2. Performance of Complete or Multiple Rocket Propulsion Systems
  • 10.3. Propellant Budget
  • 10.4. Engine Design
  • 10.5. Engine Controls
  • 10.6. Engine System Calibration
  • 10.7. System Integration and Engine Optimization
  • Problems
  • Symbols
  • References
• 11. Solid Propellant Rocket Fundamentals
  • 11.1. Propellant Burning Rate
  • 11.2. Basic Performance Relations
  • 11.3. Propellant Grain and Grain Configuration
  • 11.4. Propellant Grain Stress and Strain
  • 11.5. Attitude Control and Side Maneuvers with Solid Propellant Rocket Motors
  • Problems
  • Symbols
  • References
• 12. Solid Propellants
  • 12.1. Classification
  • 12.2. Propellant Characteristics
  • 12.3. Hazards
  • 12.4. Propellant Ingredients
  • 12.5. Other Propellant Categories
  • 12.6. Liners, Insulators, and Inhibitors
  • 12.7. Propellant Processing and Manufacture
  • Problems
  • References
• 13. Combustion of Solid Propellants
  • 13.1. Physical and Chemical Processes
  • 13.2. Ignition Process
  • 13.3. Extinction or Thrust Termination
  • 13.4. Combustion Instability
  • Problems
  • References
• 14. Solid Rocket Components and Motor Design
  • 14.1. Motor Case
  • 14.2. Nozzle
  • 14.3. Igniter Hardware
  • 14.4. Rocket Motor Design Approach
  • Problems
  • References
• 15. Hybrid Propellant Rockets
  • 15.1. Applications and Propellants
  • 15.2. Performance Analysis and Grain Configuration
  • 15.3. Design Example
  • 15.4. Combustion Instability
  • Symbols
  • References
• 16. Thrust Vector Control
  • 16.1. TVC Mechanisms with a Single Nozzle
  • 16.2. TVC with Multiple Thrust Chambers or Nozzles
  • 16.3. Testing
  • 16.4. Integration with Vehicle
  • References
• 17. Selection of Rocket Propulsion Systems
  • 17.1. Selection Process
  • 17.2. Criteria for Selection
  • 17.3. Interfaces
  • References
• 18. Rocket Exhaust Plumes
  • 18.1 Plume Appearance and Flow Behavior
  • 18.2. Plume Effects
  • 18.3. Analysis and Mathematical Simulation
  • Problems
  • References
• 19. Electric Propulsion
  • 19.1. Ideal Flight Performance
  • 19.2. Electrothermal Thrusters
  • 19.3. Non-Thermal Electric Thrusters
  • 19.4. Optimum Flight Performance
  • 19.5. Mission Applications
  • 19.6. Electric Space-Power Supplies and Power-Conditioning Systems
  • Problems
  • Symbols
  • References
• 20. Rocket Testing
  • 20.1. Types of Tests
  • 20.2. Test Facilities and Safeguards
  • 20.3. Instrumentation and Data Management
  • 20.4. Flight Testing
  • 20.5. Postaccident Procedures
  • References
• Appendix 1: Conversion Factors and Constants
• Appendix 2: Properties of the Earth's Standard Atmosphere
• Appendix 3: Summary of Key Equations for Ideal Chemical Rockets
• Appendix 4: Derivation of Hybrid Fuel Regression Rate Equation in Chapter 15
• Appendix 5: Alternative Interpretations of Boundary Layer Blowing Coefficient in Chapter 15
• Index
  • A
  • B
  • C
  • D
  • E
  • F
  • G
  • H
  • I
  • J
  • K
  • L
  • M
  • N
  • O
  • P
  • Q
  • R
  • S
  • T
  • U
  • V
  • W
  • X
  • Y

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